Patent classifications
H01B7/043
Electric energy transmission tether for an airborne wind power station
An electric energy transmission tether for an airborne wind power station comprises an elastic core, a first layer of one or more electric conductors helically wound around the elastic core, an electric insulation layer surrounding the first layer of electric conductors, a second layer of one or more electric conductors helically wound around the electric insulation layer, and a load bearing layer surrounding the second layer of electric conductors, for absorbing tensile forces and radial pressure forces acting on the tether.
Tethers for airborne wind turbines using electrical conductor bundles
A tether may include a core, a hybrid layer surrounding the core, and a jacket surrounding the hybrid layer. The hybrid layer may include a plurality of strength members, and a plurality of electrical conductor bundles. Each electrical conductor bundle of the plurality of electrical bundles may include a compliant element, a plurality of electrical conducting elements surrounding the compliant element, and an insulating layer surrounding the plurality of electrical conducting elements.
Torsion Relieving Power Cable
Disclosed herein is a power cable that includes a first conductor guide that includes (i) a first distal receiving hole and (ii) a first axial receiving hole on a longitudinal axis of the power cable. The power cable also includes a second conductor guide that includes (i) a second distal receiving hole and (ii) a second axial receiving hole on the longitudinal axis. The power cable also includes a flexible drive shaft that is disposed in the first axial receiving hole and the second axial receiving hole and a conductor that twists around the longitudinal axis. The conductor is disposed in the first distal receiving hole and the second distal receiving hole. Methods for forming the power cable are also disclosed herein.
Tethers for airborne wind turbines
A tether may include a core, a plurality of electrical conductors wound around the core, and a jacket surrounding the plurality of electrical conductors. The plurality of electrical conductors may include at least two groups of electrical conductors. Each group of electrical conductors of the at least two groups of electrical conductors may define a respective electrical path, where the respective electrical path is different from the electrical paths defined by other groups of electrical conductors of the at least two groups of the electrical conductors. Moreover, each group of electrical conductors of the at least two groups of electrical conductors is located around a respective portion of the core, such that a cross-section of each group of electrical conductors of the at least two or more electrical conductors defines a respective arc around the respective portion of the core.
Tethers for Airborne Wind Turbines Using Electrical Conductor Bundles
A tether may include a core, a hybrid layer surrounding the core, and a jacket surrounding the hybrid layer. The hybrid layer may include a plurality of strength members, and a plurality of electrical conductor bundles. Each electrical conductor bundle of the plurality of electrical bundles may include a compliant element, a plurality of electrical conducting elements surrounding the compliant element, and an insulating layer surrounding the plurality of electrical conducting elements.
Electro-Mechanical Bridles for Energy Kites
An energy kite may be coupled to a tether and ground station via an electro-mechanical bridle. The energy kite may generate a significant amount of lift during power generation and may need to transfer this load to a tether that is anchored at the ground. Transferring the load at a single point would place a substantial bending moment on the energy kite. To mitigate this bending moment, the load may be divided between multiple locations with a bridle system. The bridle system may have a plurality of electrical conductors to conduct electrical power and signals.
Electrical cable for the aerospace field
An insulated electrically conductive element (1) for the aerospace field has an elongate electrically conductive element surrounded by at least two layers, said two layers being an electrically insulating layer (4) surrounding the elongate electrically conductive element (2) and a first semiconductor layer (5) surrounding said electrically insulating layer (4), at least one of the layers having at least one fluoropolymer.